Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K

Frolov, S.; Zvegintsev, V.; Ivanov, V.; Aksenov, V.; Shamshin, I.; Vnuchkov, D.; Nalivaichenko, D.; Berlin, A.; Fomin, V.; Shiplyuk, A.; Yakovlev, N.

doi:10.31857/S086956520001377-7

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Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K

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Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K

PII

S086956520001377-7-1

DOI

10.31857/S086956520001377-7

Publication type

Article

Status

Published

Authors

S. Frolov

Affiliation:

V. Zvegintsev

Affiliation:

V. Ivanov

Affiliation:

V. Aksenov

Affiliation:

I. Shamshin

Affiliation:

D. Vnuchkov

Affiliation:

D. Nalivaichenko

Affiliation:

A. Berlin

Affiliation:

V. Fomin

Affiliation:

A. Shiplyuk

Affiliation:

N. Yakovlev

Affiliation:

Journal name

Doklady Akademii nauk

Edition

Pages

276-280

Abstract

Keywords

Received

14.10.2018

Publication date

16.10.2018

Number of characters

368

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GOST	Frolov S., Zvegintsev V., Ivanov V., Aksenov V., Shamshin I., Vnuchkov D., Nalivaichenko D., Berlin A., Fomin V., Shiplyuk A., Yakovlev N. Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K // Doklady Akademii nauk – 2018. – V. 481. – Issue 3 C. 276-280 [Electronic resource]. URL: http://ras.jes.su/dan/s207987840000616-6-1-en (circulation date: 09.10.2024). DOI: 10.31857/S086956520001377-7
MLA	Frolov, S., Zvegintsev, V., Ivanov, V., Aksenov, V., Shamshin, I., Vnuchkov, D., Nalivaichenko, D., Berlin, A., Fomin, V., Shiplyuk, A., Yakovlev, N. "Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K." Doklady Akademii nauk 481.3 (2018):276-280. DOI: 10.31857/S086956520001377-7
APA	Frolov S., Zvegintsev V., Ivanov V., Aksenov V., Shamshin I., Vnuchkov D., Nalivaichenko D., Berlin A., Fomin V., Shiplyuk A., Yakovlev N. (2018). Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K. Doklady Akademii nauk 481(3), pp.276-280 DOI: 10.31857/S086956520001377-7

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